View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 50828U 26145.51640101 +.00000000 +00000-0 +49936-4 0 00007
2 50828 53.2148 184.1260 0001127 102.7350 257.3768 15.08840001 04
| Epoch (UTC): | 25 May 2026 12:23:37 |
| Eccentricity: | 0.0001127 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 184.1260° |
| argument of perigee: | 102.7350° |
| revolutions per day: | 15.08840001 |
| mean anomaly at epoch: | 257.3768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|